An aircraft landing gear wheel is disclosed. A main body includes a hub portion with a gear end and an attachment end. A driven gear portion includes a first annular rail and a second annular rail, the driven gear portion being integrally and drivingly connected with the hub portion at the gear end. Rollers are rotatingly connected between roller apertures of the first annular rail and the second annular rail. Bearings rotatingly support portions of the rollers within the roller apertures.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft landing gear wheel with integral gear drive


    Contributors:

    Publication date :

    2016-11-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT LANDING GEAR WHEEL WITH INTEGRAL GEAR DRIVE

    CHRISTENSEN DONALD JEFFREY / MITCHELL ROBERT | European Patent Office | 2016

    Free access

    AIRCRAFT LANDING GEAR WHEEL WITH INTEGRAL GEAR DRIVE

    CHRISTENSEN DONALD JEFFREY / MITCHELL ROBERT | European Patent Office | 2016

    Free access

    Aircraft landing gear wheel-drive system

    LO CHARLES / STEVES ALLAN | European Patent Office | 2017

    Free access

    AIRCRAFT LANDING GEAR WHEEL-DRIVE SYSTEM

    LO CHARLES / STEVES ALLAN | European Patent Office | 2017

    Free access

    Aircraft landing gear drive wheel identification system

    JAN VANA / JOSEPH J COX / ISAIAH W COX et al. | European Patent Office | 2017

    Free access